View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 33376U 26145.01294634 +.00000000 +00000-0 +00000-0 0 00002
2 33376 0.0471 104.5742 0002913 326.5315 79.1700 1.00273197 03
| Epoch (UTC): | 25 May 2026 00:18:38 |
| Eccentricity: | 0.0002913 |
| inclination: | 0.0471° |
| perigee height: | 35774 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 104.5742° |
| argument of perigee: | 326.5315° |
| revolutions per day: | 1.00273197 |
| mean anomaly at epoch: | 79.1700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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